Construction of the initial deorbit region for landing at the given place
- Authors: Evdokimov S.N.1,2, Klimanov S.I.1,2, Korchagin A.N.1,2, Mikrin E.A.1,2, Sikharulidze Y.G.1,2, Tuchin A.G.1,2
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Affiliations:
- Keldysh Institute of Applied Mathematics
- Korolev Rocket and Space Corporation Energia
- Issue: Vol 56, No 2 (2017)
- Pages: 300-310
- Section: Control Systems of Moving Objects
- URL: https://journals.rcsi.science/1064-2307/article/view/219861
- DOI: https://doi.org/10.1134/S106423071702006X
- ID: 219861
Cite item
Abstract
The algorithm of the two-point boundary problem is developed for choice the nominal deorbit point, from which a descent vehicle is enabled to land at a given place without a cross-range maneuver. The method is suggested and the example is given of constructing the initial deorbit region for landing at the Vostochny cosmodrome.
About the authors
S. N. Evdokimov
Keldysh Institute of Applied Mathematics; Korolev Rocket and Space Corporation Energia
Email: sikh@kiam1.rssi.ru
Russian Federation, Moscow; Moscow
S. I. Klimanov
Keldysh Institute of Applied Mathematics; Korolev Rocket and Space Corporation Energia
Author for correspondence.
Email: sikh@kiam1.rssi.ru
Russian Federation, Moscow; Moscow
A. N. Korchagin
Keldysh Institute of Applied Mathematics; Korolev Rocket and Space Corporation Energia
Email: sikh@kiam1.rssi.ru
Russian Federation, Moscow; Moscow
E. A. Mikrin
Keldysh Institute of Applied Mathematics; Korolev Rocket and Space Corporation Energia
Email: sikh@kiam1.rssi.ru
Russian Federation, Moscow; Moscow
Yu. G. Sikharulidze
Keldysh Institute of Applied Mathematics; Korolev Rocket and Space Corporation Energia
Email: sikh@kiam1.rssi.ru
Russian Federation, Moscow; Moscow
A. G. Tuchin
Keldysh Institute of Applied Mathematics; Korolev Rocket and Space Corporation Energia
Email: sikh@kiam1.rssi.ru
Russian Federation, Moscow; Moscow